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An-24 (Coke) Russian Transport/Passenger Aircraft

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Basic Information
Name
An-24 (Coke) Russian Transport/Passenger Aircraft
Designation
Alternate Designation
Equipment Type
Manufacturer
Antonov
Date of Introduction
1962
Description

The Antonov An-24 (Russian/Ukrainian: Антонов Ан-24) (NATO reporting name: Coke) is a 44-seat twin-turboprop transport/passenger aircraft designed in 1957 in the Soviet Union by the Antonov Design Bureau and manufactured by Kiev, Irkutsk and Ulan-Ude Aviation Factories. First flown in 1959, the An-24 was produced in some 1,000 units of various versions; in 2019 there are 109 still in service worldwide, mostly in the CIS and Africa. It was designed to replace the veteran piston Ilyushin Il-14 transport on short to medium-haul trips, optimized for operating from rough strips and unprepared airports in remote locations. The high-wing layout protects engines and blades from debris, the power-to-weight ratio is higher than that of many comparable aircraft and the machine is rugged, requiring minimal ground support equipment. Due to its rugged airframe and good performance, the An-24 was adapted to perform many secondary missions such as ice reconnaissance and engine/propeller test-bed, as well as further development to produce the An-26 tactical transport, An-30 photo-mapping/survey aircraft, and An-32 tactical transport with more powerful engines. Various projects were envisaged such as a four jet short/medium-haul airliner and various iterations of the power plant. The main production line was at the Kiev-Svyatoshino (now "Aviant") aircraft production plant which built in 1985, with 180 built at Ulan Ude and a further 197 An-24T tactical transport/freighters at Irkutsk. Production in the USSR was shut down by 1978. Production continues at China's Xi'an Aircraft Industrial Corporation which makes licensed, reverse-engineered, and redesigned aircraft as the Xian Y-7, and its derivatives. Manufacture of the Y-7, in civil form, has now been supplanted by the MA60 derivative with western engines and avionics, to improve performance and economy, and widen the export appeal.

Air & Air Defense Specifications
Crew 2
Engine Turboprop (2550 hp)
Max Speed 500.0 km/h
Cruise Speed 450.0 km/h
Wingspan 29.20 m
Variants
An-24 Original design and prototypes. Twin-engine 44-seat transport aircraft.
An-24A Airliner project powered by Kuznetsov NK-4 turboprops, discontinued when the NK-4 was canceled (first use). Production 50-seat airliners built at Kiev with the APU exhaust moved to the tip of the starboard nacelle (second use).
An-24ALK (Avtomatizeerovannaya [sistema] Lyotnovo Kontrolya – automatic flight check system) Several An-24s were converted for navigation aides calibration tasks, with one An-24LR 'Toros' re-designated An-24ALK after conversion. This aircraft was fitted with a photo-theodolite and powerful light sources for the optical sensors.
An-24AT A 1962 project for a Tactical transport with rear loading ramp and powered by Isotov TV2-117DS coupled turboprops.
AT-RD and AT-U Variants The An-24AT-RD (RD – Reaktivnyye Dvigateli – jet engines) was a tactical transport project with two turbojet boosters pod-mounted under the outer wings and a wider loading ramp. The An-24AT-U (Uskoriteli – boosters)project had three or five PRD-63 (Porokhovoy Raketnyy Dvigatel – gunpowder rocket engine) Jet Assisted Take-off (JATO) bottles, wider cargo ramp, and provision for up to three brake parachutes.
An-24B The second 50-seat airliner version with one extra window on each side, single-slotted flaps replacing the double-slotted flaps and extended chord of the center-section to compensate for the lower performance flaps. Some aircraft were delivered with four extra fuel bladders in the wing center section.
An-24D A projected long-range airliner version of the An-24B with a single RU-19 booster jet engine in the starboard nacelle, stretched fuselage with seating for 60, strengthened structure, and increased fuel capacity.
An-24LL (Letyushchaya Laboratoriya – flying laboratory) The generic suffix LL can be applied to any test-bed, but in the An-24 case seems to refer to a single aircraft equipped for metrology (the science of measurement), to be used for checking the airworthiness of production aircraft.
An-24LP (LesoPozharnyy – forest firefighter) Three An-24RV aircraft converted into fire bombers/cloud seeders by installing a tank in the cabin, optical smoke and flame detectors, provision for a thermal imager, racks for carrying flare dispensers, and the ability to carry firefighters for para-dropping.
An-24LR 'Toros' (Ice Hummock) (Ledovyy Razvedchik – ice reconnaissance) An-24Bs converted to carry the 'Toros' SLAR (sideways looking airborne radar) either side of the lower fuselage, for ice reconnaissance, guiding icebreakers, convoys, and other shipping.
"Boosted" Jet Variants An-24RT (Reaktivnyy [Uskoritel'] Transportnyy – boosted transport), which is similar to the AN-24T, fitted with an auxiliary turbojet engine. The An-24RV (Reaktivnyy [Uskoritel'] V – boosted V) is a turbojet boosted export version, similar to the An-24V but fitted with a 1,985-lb (8830 N) thrust auxiliary turbojet engine in the starboard nacelle.
An-24RT (Comms Relay) The An-24RT (Retranslyator – relay installation) project to a few An-24T and An-24RT aircraft converted to communications relay aircraft. Sometimes referred to as An-24Rt to differentiate from the An-24RT.
System
Alternate Designation(s) AN-24; NATO: Coke
Primary Function / Type Transport/Cargo Aircraft
Manufacturer Antonov
Crew 2 (pilot, co-pilot)
Passengers 50 passengers
Number of Engines 2 ea
Number of Hard Points INA
Dimensions
Length 23.53 m
Height 8.32 m
Wingspan 29.20 m
Cabin Length 9.69 m
Cabin Width 2.76 m
Cabin Height 1.91 m
Wing Area 74.98 sq m
Weight, Empty 13,300 kg
Weight, Maximum Payload 5,500 kg
Weight, Maximum Takeoff 21,000 kg
Automotive
Engine Name 2 x Ivchenko AI-24V
Number of Engines 2
Engine Type Turboprop
Engine Power 2,550 equivalent shp each
Internal Fuel Capacity 5,550 liters
Maximum Speed 500 km/h
Cruise Speed 450 km/h
Landing Speed 165 km/h
Climb Rate 114 m/min
Ceiling 8,400 m
Range, Maximum Payload 550 km
Range, Maximum Fuel, with 30 Passengers 2,400 km
Fire Control / Avionics
Fire Control System Type INA
Fire Control Radar INA
Laser Desingator INA
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares Yes
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
A
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
23.53 m
Width
Height
8.32 m
Weight
21000 kg
Operators (11)
Russia
Ukraine
North Korea
Belarus
Cambodia
Congo, Republic of the
Cuba
Mali
Mongolia
Syria
Uzbekistan
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